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Estimating Aircraft Fuel Flow for a Three-Degree Flight-Path-Angle Descent

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dc.contributor.authorTurgut, Enis T.
dc.contributor.orcid0000-0002-9601-2318
dc.date.accessioned2025-11-13T10:10:35Z
dc.date.issued2011-05-01
dc.identifier.doihttps://doi.org/10.2514/1.c031260
dc.identifier.endpage1106
dc.identifier.issn0021-8669
dc.identifier.issue3
dc.identifier.openalexW2054476390
dc.identifier.startpage1099
dc.identifier.urihttps://hdl.handle.net/11421/3356
dc.identifier.urihttps://doi.org/10.2514/1.c031260
dc.identifier.volume48
dc.language.isoen
dc.relation.ispartofJournal of Aircraft
dc.rightsrestrictedAccess
dc.subjectDescent (aeronautics)
dc.subjectAltitude (triangle)
dc.subjectContext (archaeology)
dc.subjectFuel efficiency
dc.subjectPath (computing)
dc.subjectComputer science
dc.subjectSimulation
dc.subjectEnvironmental science
dc.subjectMathematics
dc.subjectAerospace engineering
dc.subjectEngineering
dc.subjectGeology
dc.subjectGeometry
dc.subject.sdg7
dc.titleEstimating Aircraft Fuel Flow for a Three-Degree Flight-Path-Angle Descent
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5037119366

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